View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 48355U 26145.01274875 +.00000000 +00000-0 +98949-4 0 00003
2 48355 53.1607 3.1329 0001297 80.0337 280.0811 15.31713255 00
| Epoch (UTC): | 25 May 2026 00:18:21 |
| Eccentricity: | 0.0001297 |
| inclination: | 53.1607° |
| perigee height: | 470 km |
| apogee height: | 472 km |
| right ascension of ascending node: | 3.1329° |
| argument of perigee: | 80.0337° |
| revolutions per day: | 15.31713255 |
| mean anomaly at epoch: | 280.0811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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